Page 1
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part I
Mathematics and Fundamentals
Closed BookNotes
November 15 2007
Thursday
100 pm - 500 pm
Enter problem number(s)
The problems are that you selected
Ordinary Differential Equations 2 problems ( ) ( )
Partial Differential Equations 2 problems ( ) ( )
Linear Algebra 2 problems ( ) ( )
Calculus 2 problems ( ) ( )
Numerical Methods 2 problems ( ) ( )
The student should select 8 problems out of 10 problems given here Write the
problem numbers that you selected in ( ) above Also circle the problems that you
choose on each problem sheet Choose at least one problem from each category
listed above Use one exam book (blue book) for each problem Include your
assigned number and NOT your name on each book Submit both exam books and
this problem sheet when you leave
QualExam-F07Fall 2007
Ordinary Differential Equation 1
1) Find the solution y(t) of the initial value problem
0 (0) 2 (0) 3y y y yprimeprime primeprimeprime primeprimeprime primeprimeprime prime+ = = = minus+ = = = minus+ = = = minus+ = = = minus
2) What are the maximum and minimum values of the solution y(t) for minusinfin lt t lt infin
Ordinary Differential Equation 2
Consider a damped spring-mass system The position from equilibrium y at a
time t is described by the equation
0452
2
=++ ydt
dy
dt
yd
The momentum for the system is given by p = dydt
For the initial conditions of y(0) = 4 p(0) = -5 find
(a) the equation describing the position y as a function of time
(b) the equation describing the momentum p as a function of time and
(c) the total energy of the system at t = 3
Partial Differential Equation 1
The differential equation to describe the transient heat conduction is given as
0 1le lex
part
part
part
part
2
2
2
20
T
x
T
y+ =
with the boundary conditions of T as
BC
00 ==part
partxat
x
T
axatHTx
T==+
part
part0
0)( == yatxfT
byaty
T==
part
part0
where H is the convective heat transfer which you can treat as a constant
Obtain an expression for the steady state temperature distribution T(xy) in a rectangular region
byax lelelele 00
y
x a
b
0
Partial Differential Equation 2
Consider a semi-infinite rod of rectangular cross section (2Ltimes2 l ) as shown in the figure below
The base temperature of the rod is θ0 and the ambient temperature is 0 The heat transfer
coefficient is large Determine the steady state temperature of the rod using separation of
variables The governing equation can be described as follows
02
2
2
2
2
2
=part
part+
part
part+
part
part
zyx
θθθ
The boundary conditions are
0)(0)0(
==part
partzyL
x
zyθ
θ
0)(0)0(
==part
partzx
y
zxlθ
θ
)(0)()0( 0 finiteyxyx =infin= θθθ
Linear Algebra 1
Let F 4real 3real be the linear mapping defined by
F(x y s t) = (x ndash y + s + t x + 2s ndash t x + y + 3s ndash 3t)
Find a basis and the dimension of the image of U of F
Show all of your work
Linear Algebra 2
Determine the equation of the circle passing through the following three points in the plane (26) (64)
and (71)
Calculus 1
A fluid flows out of a region bounded by the curve 6x2 + 4 y
2 = 24 The velocity
field of the fluid is defined by
F(xy) = (3y + y2 + 8x) I + (x
4 ndash x + 6y ndash 3) j
Find the rate of flow out of the region The velocity is measured in cms and the
area is measured in cm2
Calculus 2
If )4(2 trnet
minus=θ what value of n will make
1 2
2 trr
rr part
part=
part
part
part
part θθ
Numerical Methods 1
Consider the typical diffusion equation
2
2
x
u
t
u
part
part=
part
part
Prove that when the following explicit scheme is used the spatial order of accuracy is second
order
2111 )21(h
krwhereruurruu jijijiji =+minus+= +minus+
Here h and k are spatial and temporal grid size What value of r should be assigned if 4th
order
spatial accuracy is required
Numerical Methods 2
Using the second-order terms of the Taylor series expansion and the forward-time and centered-
space differencing show that the advection equation
0=part
part+
part
part
x
fu
t
f (1)
can be formulated as
( )n
i
n
i
n
i
n
i
n
i
n
i
n
i fffc
ffc
ff 11
2
11
1 22
)(2
minus+minus++ +minus+minusminus=
where
x
tuc
∆
∆=
What is the order of the accuracy
Using von Neumann stability analysis determine the stability condition
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Thermal Science Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Fluid Mechanics 3 problems ( ) ( ) ( )
Thermodynamics 3 problems ( ) ( ) ( )
Heat Transfer 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your assigned number and
NOT your name on each book Submit both exam books and this problem sheet when
you leave
QualExam-F07Fall 2007
Fluid Mechanics 1
A cylindrical annular flow with the inner cylinder rotating at a constant speed ωωωω and
the outer cylinder stationary is shown in the figure below The radii of the outer and
inner cylinders are Ro and Ri respectively
(1) Express the velocity along the wall in terms of the dimensions rotating
speed=ωωωω and the fluid properties viscosity=micromicromicromicro and density=ρρρρ
(2) What is the power needed to move per unit depth Assume Ro ndash Ri ltlt Ro
(3) For SAE 30 oil at 20oC with Ro=10cm Ri=9cm and ωωωω=900rpm calculate
the power
[Hint] The equi-dimensional ordinary differential equation of the function fI
frdquo + (1r)frsquo ndash(1r2)f = 0
has a form of the general solution in the form of f1=C1r and f2=C2r
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 2
Ordinary Differential Equation 1
1) Find the solution y(t) of the initial value problem
0 (0) 2 (0) 3y y y yprimeprime primeprimeprime primeprimeprime primeprimeprime prime+ = = = minus+ = = = minus+ = = = minus+ = = = minus
2) What are the maximum and minimum values of the solution y(t) for minusinfin lt t lt infin
Ordinary Differential Equation 2
Consider a damped spring-mass system The position from equilibrium y at a
time t is described by the equation
0452
2
=++ ydt
dy
dt
yd
The momentum for the system is given by p = dydt
For the initial conditions of y(0) = 4 p(0) = -5 find
(a) the equation describing the position y as a function of time
(b) the equation describing the momentum p as a function of time and
(c) the total energy of the system at t = 3
Partial Differential Equation 1
The differential equation to describe the transient heat conduction is given as
0 1le lex
part
part
part
part
2
2
2
20
T
x
T
y+ =
with the boundary conditions of T as
BC
00 ==part
partxat
x
T
axatHTx
T==+
part
part0
0)( == yatxfT
byaty
T==
part
part0
where H is the convective heat transfer which you can treat as a constant
Obtain an expression for the steady state temperature distribution T(xy) in a rectangular region
byax lelelele 00
y
x a
b
0
Partial Differential Equation 2
Consider a semi-infinite rod of rectangular cross section (2Ltimes2 l ) as shown in the figure below
The base temperature of the rod is θ0 and the ambient temperature is 0 The heat transfer
coefficient is large Determine the steady state temperature of the rod using separation of
variables The governing equation can be described as follows
02
2
2
2
2
2
=part
part+
part
part+
part
part
zyx
θθθ
The boundary conditions are
0)(0)0(
==part
partzyL
x
zyθ
θ
0)(0)0(
==part
partzx
y
zxlθ
θ
)(0)()0( 0 finiteyxyx =infin= θθθ
Linear Algebra 1
Let F 4real 3real be the linear mapping defined by
F(x y s t) = (x ndash y + s + t x + 2s ndash t x + y + 3s ndash 3t)
Find a basis and the dimension of the image of U of F
Show all of your work
Linear Algebra 2
Determine the equation of the circle passing through the following three points in the plane (26) (64)
and (71)
Calculus 1
A fluid flows out of a region bounded by the curve 6x2 + 4 y
2 = 24 The velocity
field of the fluid is defined by
F(xy) = (3y + y2 + 8x) I + (x
4 ndash x + 6y ndash 3) j
Find the rate of flow out of the region The velocity is measured in cms and the
area is measured in cm2
Calculus 2
If )4(2 trnet
minus=θ what value of n will make
1 2
2 trr
rr part
part=
part
part
part
part θθ
Numerical Methods 1
Consider the typical diffusion equation
2
2
x
u
t
u
part
part=
part
part
Prove that when the following explicit scheme is used the spatial order of accuracy is second
order
2111 )21(h
krwhereruurruu jijijiji =+minus+= +minus+
Here h and k are spatial and temporal grid size What value of r should be assigned if 4th
order
spatial accuracy is required
Numerical Methods 2
Using the second-order terms of the Taylor series expansion and the forward-time and centered-
space differencing show that the advection equation
0=part
part+
part
part
x
fu
t
f (1)
can be formulated as
( )n
i
n
i
n
i
n
i
n
i
n
i
n
i fffc
ffc
ff 11
2
11
1 22
)(2
minus+minus++ +minus+minusminus=
where
x
tuc
∆
∆=
What is the order of the accuracy
Using von Neumann stability analysis determine the stability condition
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Thermal Science Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Fluid Mechanics 3 problems ( ) ( ) ( )
Thermodynamics 3 problems ( ) ( ) ( )
Heat Transfer 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your assigned number and
NOT your name on each book Submit both exam books and this problem sheet when
you leave
QualExam-F07Fall 2007
Fluid Mechanics 1
A cylindrical annular flow with the inner cylinder rotating at a constant speed ωωωω and
the outer cylinder stationary is shown in the figure below The radii of the outer and
inner cylinders are Ro and Ri respectively
(1) Express the velocity along the wall in terms of the dimensions rotating
speed=ωωωω and the fluid properties viscosity=micromicromicromicro and density=ρρρρ
(2) What is the power needed to move per unit depth Assume Ro ndash Ri ltlt Ro
(3) For SAE 30 oil at 20oC with Ro=10cm Ri=9cm and ωωωω=900rpm calculate
the power
[Hint] The equi-dimensional ordinary differential equation of the function fI
frdquo + (1r)frsquo ndash(1r2)f = 0
has a form of the general solution in the form of f1=C1r and f2=C2r
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 3
Ordinary Differential Equation 2
Consider a damped spring-mass system The position from equilibrium y at a
time t is described by the equation
0452
2
=++ ydt
dy
dt
yd
The momentum for the system is given by p = dydt
For the initial conditions of y(0) = 4 p(0) = -5 find
(a) the equation describing the position y as a function of time
(b) the equation describing the momentum p as a function of time and
(c) the total energy of the system at t = 3
Partial Differential Equation 1
The differential equation to describe the transient heat conduction is given as
0 1le lex
part
part
part
part
2
2
2
20
T
x
T
y+ =
with the boundary conditions of T as
BC
00 ==part
partxat
x
T
axatHTx
T==+
part
part0
0)( == yatxfT
byaty
T==
part
part0
where H is the convective heat transfer which you can treat as a constant
Obtain an expression for the steady state temperature distribution T(xy) in a rectangular region
byax lelelele 00
y
x a
b
0
Partial Differential Equation 2
Consider a semi-infinite rod of rectangular cross section (2Ltimes2 l ) as shown in the figure below
The base temperature of the rod is θ0 and the ambient temperature is 0 The heat transfer
coefficient is large Determine the steady state temperature of the rod using separation of
variables The governing equation can be described as follows
02
2
2
2
2
2
=part
part+
part
part+
part
part
zyx
θθθ
The boundary conditions are
0)(0)0(
==part
partzyL
x
zyθ
θ
0)(0)0(
==part
partzx
y
zxlθ
θ
)(0)()0( 0 finiteyxyx =infin= θθθ
Linear Algebra 1
Let F 4real 3real be the linear mapping defined by
F(x y s t) = (x ndash y + s + t x + 2s ndash t x + y + 3s ndash 3t)
Find a basis and the dimension of the image of U of F
Show all of your work
Linear Algebra 2
Determine the equation of the circle passing through the following three points in the plane (26) (64)
and (71)
Calculus 1
A fluid flows out of a region bounded by the curve 6x2 + 4 y
2 = 24 The velocity
field of the fluid is defined by
F(xy) = (3y + y2 + 8x) I + (x
4 ndash x + 6y ndash 3) j
Find the rate of flow out of the region The velocity is measured in cms and the
area is measured in cm2
Calculus 2
If )4(2 trnet
minus=θ what value of n will make
1 2
2 trr
rr part
part=
part
part
part
part θθ
Numerical Methods 1
Consider the typical diffusion equation
2
2
x
u
t
u
part
part=
part
part
Prove that when the following explicit scheme is used the spatial order of accuracy is second
order
2111 )21(h
krwhereruurruu jijijiji =+minus+= +minus+
Here h and k are spatial and temporal grid size What value of r should be assigned if 4th
order
spatial accuracy is required
Numerical Methods 2
Using the second-order terms of the Taylor series expansion and the forward-time and centered-
space differencing show that the advection equation
0=part
part+
part
part
x
fu
t
f (1)
can be formulated as
( )n
i
n
i
n
i
n
i
n
i
n
i
n
i fffc
ffc
ff 11
2
11
1 22
)(2
minus+minus++ +minus+minusminus=
where
x
tuc
∆
∆=
What is the order of the accuracy
Using von Neumann stability analysis determine the stability condition
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Thermal Science Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Fluid Mechanics 3 problems ( ) ( ) ( )
Thermodynamics 3 problems ( ) ( ) ( )
Heat Transfer 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your assigned number and
NOT your name on each book Submit both exam books and this problem sheet when
you leave
QualExam-F07Fall 2007
Fluid Mechanics 1
A cylindrical annular flow with the inner cylinder rotating at a constant speed ωωωω and
the outer cylinder stationary is shown in the figure below The radii of the outer and
inner cylinders are Ro and Ri respectively
(1) Express the velocity along the wall in terms of the dimensions rotating
speed=ωωωω and the fluid properties viscosity=micromicromicromicro and density=ρρρρ
(2) What is the power needed to move per unit depth Assume Ro ndash Ri ltlt Ro
(3) For SAE 30 oil at 20oC with Ro=10cm Ri=9cm and ωωωω=900rpm calculate
the power
[Hint] The equi-dimensional ordinary differential equation of the function fI
frdquo + (1r)frsquo ndash(1r2)f = 0
has a form of the general solution in the form of f1=C1r and f2=C2r
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 4
Partial Differential Equation 1
The differential equation to describe the transient heat conduction is given as
0 1le lex
part
part
part
part
2
2
2
20
T
x
T
y+ =
with the boundary conditions of T as
BC
00 ==part
partxat
x
T
axatHTx
T==+
part
part0
0)( == yatxfT
byaty
T==
part
part0
where H is the convective heat transfer which you can treat as a constant
Obtain an expression for the steady state temperature distribution T(xy) in a rectangular region
byax lelelele 00
y
x a
b
0
Partial Differential Equation 2
Consider a semi-infinite rod of rectangular cross section (2Ltimes2 l ) as shown in the figure below
The base temperature of the rod is θ0 and the ambient temperature is 0 The heat transfer
coefficient is large Determine the steady state temperature of the rod using separation of
variables The governing equation can be described as follows
02
2
2
2
2
2
=part
part+
part
part+
part
part
zyx
θθθ
The boundary conditions are
0)(0)0(
==part
partzyL
x
zyθ
θ
0)(0)0(
==part
partzx
y
zxlθ
θ
)(0)()0( 0 finiteyxyx =infin= θθθ
Linear Algebra 1
Let F 4real 3real be the linear mapping defined by
F(x y s t) = (x ndash y + s + t x + 2s ndash t x + y + 3s ndash 3t)
Find a basis and the dimension of the image of U of F
Show all of your work
Linear Algebra 2
Determine the equation of the circle passing through the following three points in the plane (26) (64)
and (71)
Calculus 1
A fluid flows out of a region bounded by the curve 6x2 + 4 y
2 = 24 The velocity
field of the fluid is defined by
F(xy) = (3y + y2 + 8x) I + (x
4 ndash x + 6y ndash 3) j
Find the rate of flow out of the region The velocity is measured in cms and the
area is measured in cm2
Calculus 2
If )4(2 trnet
minus=θ what value of n will make
1 2
2 trr
rr part
part=
part
part
part
part θθ
Numerical Methods 1
Consider the typical diffusion equation
2
2
x
u
t
u
part
part=
part
part
Prove that when the following explicit scheme is used the spatial order of accuracy is second
order
2111 )21(h
krwhereruurruu jijijiji =+minus+= +minus+
Here h and k are spatial and temporal grid size What value of r should be assigned if 4th
order
spatial accuracy is required
Numerical Methods 2
Using the second-order terms of the Taylor series expansion and the forward-time and centered-
space differencing show that the advection equation
0=part
part+
part
part
x
fu
t
f (1)
can be formulated as
( )n
i
n
i
n
i
n
i
n
i
n
i
n
i fffc
ffc
ff 11
2
11
1 22
)(2
minus+minus++ +minus+minusminus=
where
x
tuc
∆
∆=
What is the order of the accuracy
Using von Neumann stability analysis determine the stability condition
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Thermal Science Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Fluid Mechanics 3 problems ( ) ( ) ( )
Thermodynamics 3 problems ( ) ( ) ( )
Heat Transfer 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your assigned number and
NOT your name on each book Submit both exam books and this problem sheet when
you leave
QualExam-F07Fall 2007
Fluid Mechanics 1
A cylindrical annular flow with the inner cylinder rotating at a constant speed ωωωω and
the outer cylinder stationary is shown in the figure below The radii of the outer and
inner cylinders are Ro and Ri respectively
(1) Express the velocity along the wall in terms of the dimensions rotating
speed=ωωωω and the fluid properties viscosity=micromicromicromicro and density=ρρρρ
(2) What is the power needed to move per unit depth Assume Ro ndash Ri ltlt Ro
(3) For SAE 30 oil at 20oC with Ro=10cm Ri=9cm and ωωωω=900rpm calculate
the power
[Hint] The equi-dimensional ordinary differential equation of the function fI
frdquo + (1r)frsquo ndash(1r2)f = 0
has a form of the general solution in the form of f1=C1r and f2=C2r
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 5
Partial Differential Equation 2
Consider a semi-infinite rod of rectangular cross section (2Ltimes2 l ) as shown in the figure below
The base temperature of the rod is θ0 and the ambient temperature is 0 The heat transfer
coefficient is large Determine the steady state temperature of the rod using separation of
variables The governing equation can be described as follows
02
2
2
2
2
2
=part
part+
part
part+
part
part
zyx
θθθ
The boundary conditions are
0)(0)0(
==part
partzyL
x
zyθ
θ
0)(0)0(
==part
partzx
y
zxlθ
θ
)(0)()0( 0 finiteyxyx =infin= θθθ
Linear Algebra 1
Let F 4real 3real be the linear mapping defined by
F(x y s t) = (x ndash y + s + t x + 2s ndash t x + y + 3s ndash 3t)
Find a basis and the dimension of the image of U of F
Show all of your work
Linear Algebra 2
Determine the equation of the circle passing through the following three points in the plane (26) (64)
and (71)
Calculus 1
A fluid flows out of a region bounded by the curve 6x2 + 4 y
2 = 24 The velocity
field of the fluid is defined by
F(xy) = (3y + y2 + 8x) I + (x
4 ndash x + 6y ndash 3) j
Find the rate of flow out of the region The velocity is measured in cms and the
area is measured in cm2
Calculus 2
If )4(2 trnet
minus=θ what value of n will make
1 2
2 trr
rr part
part=
part
part
part
part θθ
Numerical Methods 1
Consider the typical diffusion equation
2
2
x
u
t
u
part
part=
part
part
Prove that when the following explicit scheme is used the spatial order of accuracy is second
order
2111 )21(h
krwhereruurruu jijijiji =+minus+= +minus+
Here h and k are spatial and temporal grid size What value of r should be assigned if 4th
order
spatial accuracy is required
Numerical Methods 2
Using the second-order terms of the Taylor series expansion and the forward-time and centered-
space differencing show that the advection equation
0=part
part+
part
part
x
fu
t
f (1)
can be formulated as
( )n
i
n
i
n
i
n
i
n
i
n
i
n
i fffc
ffc
ff 11
2
11
1 22
)(2
minus+minus++ +minus+minusminus=
where
x
tuc
∆
∆=
What is the order of the accuracy
Using von Neumann stability analysis determine the stability condition
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Thermal Science Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Fluid Mechanics 3 problems ( ) ( ) ( )
Thermodynamics 3 problems ( ) ( ) ( )
Heat Transfer 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your assigned number and
NOT your name on each book Submit both exam books and this problem sheet when
you leave
QualExam-F07Fall 2007
Fluid Mechanics 1
A cylindrical annular flow with the inner cylinder rotating at a constant speed ωωωω and
the outer cylinder stationary is shown in the figure below The radii of the outer and
inner cylinders are Ro and Ri respectively
(1) Express the velocity along the wall in terms of the dimensions rotating
speed=ωωωω and the fluid properties viscosity=micromicromicromicro and density=ρρρρ
(2) What is the power needed to move per unit depth Assume Ro ndash Ri ltlt Ro
(3) For SAE 30 oil at 20oC with Ro=10cm Ri=9cm and ωωωω=900rpm calculate
the power
[Hint] The equi-dimensional ordinary differential equation of the function fI
frdquo + (1r)frsquo ndash(1r2)f = 0
has a form of the general solution in the form of f1=C1r and f2=C2r
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 6
Linear Algebra 1
Let F 4real 3real be the linear mapping defined by
F(x y s t) = (x ndash y + s + t x + 2s ndash t x + y + 3s ndash 3t)
Find a basis and the dimension of the image of U of F
Show all of your work
Linear Algebra 2
Determine the equation of the circle passing through the following three points in the plane (26) (64)
and (71)
Calculus 1
A fluid flows out of a region bounded by the curve 6x2 + 4 y
2 = 24 The velocity
field of the fluid is defined by
F(xy) = (3y + y2 + 8x) I + (x
4 ndash x + 6y ndash 3) j
Find the rate of flow out of the region The velocity is measured in cms and the
area is measured in cm2
Calculus 2
If )4(2 trnet
minus=θ what value of n will make
1 2
2 trr
rr part
part=
part
part
part
part θθ
Numerical Methods 1
Consider the typical diffusion equation
2
2
x
u
t
u
part
part=
part
part
Prove that when the following explicit scheme is used the spatial order of accuracy is second
order
2111 )21(h
krwhereruurruu jijijiji =+minus+= +minus+
Here h and k are spatial and temporal grid size What value of r should be assigned if 4th
order
spatial accuracy is required
Numerical Methods 2
Using the second-order terms of the Taylor series expansion and the forward-time and centered-
space differencing show that the advection equation
0=part
part+
part
part
x
fu
t
f (1)
can be formulated as
( )n
i
n
i
n
i
n
i
n
i
n
i
n
i fffc
ffc
ff 11
2
11
1 22
)(2
minus+minus++ +minus+minusminus=
where
x
tuc
∆
∆=
What is the order of the accuracy
Using von Neumann stability analysis determine the stability condition
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Thermal Science Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Fluid Mechanics 3 problems ( ) ( ) ( )
Thermodynamics 3 problems ( ) ( ) ( )
Heat Transfer 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your assigned number and
NOT your name on each book Submit both exam books and this problem sheet when
you leave
QualExam-F07Fall 2007
Fluid Mechanics 1
A cylindrical annular flow with the inner cylinder rotating at a constant speed ωωωω and
the outer cylinder stationary is shown in the figure below The radii of the outer and
inner cylinders are Ro and Ri respectively
(1) Express the velocity along the wall in terms of the dimensions rotating
speed=ωωωω and the fluid properties viscosity=micromicromicromicro and density=ρρρρ
(2) What is the power needed to move per unit depth Assume Ro ndash Ri ltlt Ro
(3) For SAE 30 oil at 20oC with Ro=10cm Ri=9cm and ωωωω=900rpm calculate
the power
[Hint] The equi-dimensional ordinary differential equation of the function fI
frdquo + (1r)frsquo ndash(1r2)f = 0
has a form of the general solution in the form of f1=C1r and f2=C2r
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 7
Linear Algebra 2
Determine the equation of the circle passing through the following three points in the plane (26) (64)
and (71)
Calculus 1
A fluid flows out of a region bounded by the curve 6x2 + 4 y
2 = 24 The velocity
field of the fluid is defined by
F(xy) = (3y + y2 + 8x) I + (x
4 ndash x + 6y ndash 3) j
Find the rate of flow out of the region The velocity is measured in cms and the
area is measured in cm2
Calculus 2
If )4(2 trnet
minus=θ what value of n will make
1 2
2 trr
rr part
part=
part
part
part
part θθ
Numerical Methods 1
Consider the typical diffusion equation
2
2
x
u
t
u
part
part=
part
part
Prove that when the following explicit scheme is used the spatial order of accuracy is second
order
2111 )21(h
krwhereruurruu jijijiji =+minus+= +minus+
Here h and k are spatial and temporal grid size What value of r should be assigned if 4th
order
spatial accuracy is required
Numerical Methods 2
Using the second-order terms of the Taylor series expansion and the forward-time and centered-
space differencing show that the advection equation
0=part
part+
part
part
x
fu
t
f (1)
can be formulated as
( )n
i
n
i
n
i
n
i
n
i
n
i
n
i fffc
ffc
ff 11
2
11
1 22
)(2
minus+minus++ +minus+minusminus=
where
x
tuc
∆
∆=
What is the order of the accuracy
Using von Neumann stability analysis determine the stability condition
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Thermal Science Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Fluid Mechanics 3 problems ( ) ( ) ( )
Thermodynamics 3 problems ( ) ( ) ( )
Heat Transfer 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your assigned number and
NOT your name on each book Submit both exam books and this problem sheet when
you leave
QualExam-F07Fall 2007
Fluid Mechanics 1
A cylindrical annular flow with the inner cylinder rotating at a constant speed ωωωω and
the outer cylinder stationary is shown in the figure below The radii of the outer and
inner cylinders are Ro and Ri respectively
(1) Express the velocity along the wall in terms of the dimensions rotating
speed=ωωωω and the fluid properties viscosity=micromicromicromicro and density=ρρρρ
(2) What is the power needed to move per unit depth Assume Ro ndash Ri ltlt Ro
(3) For SAE 30 oil at 20oC with Ro=10cm Ri=9cm and ωωωω=900rpm calculate
the power
[Hint] The equi-dimensional ordinary differential equation of the function fI
frdquo + (1r)frsquo ndash(1r2)f = 0
has a form of the general solution in the form of f1=C1r and f2=C2r
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 8
Calculus 1
A fluid flows out of a region bounded by the curve 6x2 + 4 y
2 = 24 The velocity
field of the fluid is defined by
F(xy) = (3y + y2 + 8x) I + (x
4 ndash x + 6y ndash 3) j
Find the rate of flow out of the region The velocity is measured in cms and the
area is measured in cm2
Calculus 2
If )4(2 trnet
minus=θ what value of n will make
1 2
2 trr
rr part
part=
part
part
part
part θθ
Numerical Methods 1
Consider the typical diffusion equation
2
2
x
u
t
u
part
part=
part
part
Prove that when the following explicit scheme is used the spatial order of accuracy is second
order
2111 )21(h
krwhereruurruu jijijiji =+minus+= +minus+
Here h and k are spatial and temporal grid size What value of r should be assigned if 4th
order
spatial accuracy is required
Numerical Methods 2
Using the second-order terms of the Taylor series expansion and the forward-time and centered-
space differencing show that the advection equation
0=part
part+
part
part
x
fu
t
f (1)
can be formulated as
( )n
i
n
i
n
i
n
i
n
i
n
i
n
i fffc
ffc
ff 11
2
11
1 22
)(2
minus+minus++ +minus+minusminus=
where
x
tuc
∆
∆=
What is the order of the accuracy
Using von Neumann stability analysis determine the stability condition
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Thermal Science Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Fluid Mechanics 3 problems ( ) ( ) ( )
Thermodynamics 3 problems ( ) ( ) ( )
Heat Transfer 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your assigned number and
NOT your name on each book Submit both exam books and this problem sheet when
you leave
QualExam-F07Fall 2007
Fluid Mechanics 1
A cylindrical annular flow with the inner cylinder rotating at a constant speed ωωωω and
the outer cylinder stationary is shown in the figure below The radii of the outer and
inner cylinders are Ro and Ri respectively
(1) Express the velocity along the wall in terms of the dimensions rotating
speed=ωωωω and the fluid properties viscosity=micromicromicromicro and density=ρρρρ
(2) What is the power needed to move per unit depth Assume Ro ndash Ri ltlt Ro
(3) For SAE 30 oil at 20oC with Ro=10cm Ri=9cm and ωωωω=900rpm calculate
the power
[Hint] The equi-dimensional ordinary differential equation of the function fI
frdquo + (1r)frsquo ndash(1r2)f = 0
has a form of the general solution in the form of f1=C1r and f2=C2r
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 9
Calculus 2
If )4(2 trnet
minus=θ what value of n will make
1 2
2 trr
rr part
part=
part
part
part
part θθ
Numerical Methods 1
Consider the typical diffusion equation
2
2
x
u
t
u
part
part=
part
part
Prove that when the following explicit scheme is used the spatial order of accuracy is second
order
2111 )21(h
krwhereruurruu jijijiji =+minus+= +minus+
Here h and k are spatial and temporal grid size What value of r should be assigned if 4th
order
spatial accuracy is required
Numerical Methods 2
Using the second-order terms of the Taylor series expansion and the forward-time and centered-
space differencing show that the advection equation
0=part
part+
part
part
x
fu
t
f (1)
can be formulated as
( )n
i
n
i
n
i
n
i
n
i
n
i
n
i fffc
ffc
ff 11
2
11
1 22
)(2
minus+minus++ +minus+minusminus=
where
x
tuc
∆
∆=
What is the order of the accuracy
Using von Neumann stability analysis determine the stability condition
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Thermal Science Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Fluid Mechanics 3 problems ( ) ( ) ( )
Thermodynamics 3 problems ( ) ( ) ( )
Heat Transfer 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your assigned number and
NOT your name on each book Submit both exam books and this problem sheet when
you leave
QualExam-F07Fall 2007
Fluid Mechanics 1
A cylindrical annular flow with the inner cylinder rotating at a constant speed ωωωω and
the outer cylinder stationary is shown in the figure below The radii of the outer and
inner cylinders are Ro and Ri respectively
(1) Express the velocity along the wall in terms of the dimensions rotating
speed=ωωωω and the fluid properties viscosity=micromicromicromicro and density=ρρρρ
(2) What is the power needed to move per unit depth Assume Ro ndash Ri ltlt Ro
(3) For SAE 30 oil at 20oC with Ro=10cm Ri=9cm and ωωωω=900rpm calculate
the power
[Hint] The equi-dimensional ordinary differential equation of the function fI
frdquo + (1r)frsquo ndash(1r2)f = 0
has a form of the general solution in the form of f1=C1r and f2=C2r
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 10
Numerical Methods 1
Consider the typical diffusion equation
2
2
x
u
t
u
part
part=
part
part
Prove that when the following explicit scheme is used the spatial order of accuracy is second
order
2111 )21(h
krwhereruurruu jijijiji =+minus+= +minus+
Here h and k are spatial and temporal grid size What value of r should be assigned if 4th
order
spatial accuracy is required
Numerical Methods 2
Using the second-order terms of the Taylor series expansion and the forward-time and centered-
space differencing show that the advection equation
0=part
part+
part
part
x
fu
t
f (1)
can be formulated as
( )n
i
n
i
n
i
n
i
n
i
n
i
n
i fffc
ffc
ff 11
2
11
1 22
)(2
minus+minus++ +minus+minusminus=
where
x
tuc
∆
∆=
What is the order of the accuracy
Using von Neumann stability analysis determine the stability condition
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Thermal Science Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Fluid Mechanics 3 problems ( ) ( ) ( )
Thermodynamics 3 problems ( ) ( ) ( )
Heat Transfer 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your assigned number and
NOT your name on each book Submit both exam books and this problem sheet when
you leave
QualExam-F07Fall 2007
Fluid Mechanics 1
A cylindrical annular flow with the inner cylinder rotating at a constant speed ωωωω and
the outer cylinder stationary is shown in the figure below The radii of the outer and
inner cylinders are Ro and Ri respectively
(1) Express the velocity along the wall in terms of the dimensions rotating
speed=ωωωω and the fluid properties viscosity=micromicromicromicro and density=ρρρρ
(2) What is the power needed to move per unit depth Assume Ro ndash Ri ltlt Ro
(3) For SAE 30 oil at 20oC with Ro=10cm Ri=9cm and ωωωω=900rpm calculate
the power
[Hint] The equi-dimensional ordinary differential equation of the function fI
frdquo + (1r)frsquo ndash(1r2)f = 0
has a form of the general solution in the form of f1=C1r and f2=C2r
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 11
Numerical Methods 2
Using the second-order terms of the Taylor series expansion and the forward-time and centered-
space differencing show that the advection equation
0=part
part+
part
part
x
fu
t
f (1)
can be formulated as
( )n
i
n
i
n
i
n
i
n
i
n
i
n
i fffc
ffc
ff 11
2
11
1 22
)(2
minus+minus++ +minus+minusminus=
where
x
tuc
∆
∆=
What is the order of the accuracy
Using von Neumann stability analysis determine the stability condition
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Thermal Science Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Fluid Mechanics 3 problems ( ) ( ) ( )
Thermodynamics 3 problems ( ) ( ) ( )
Heat Transfer 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your assigned number and
NOT your name on each book Submit both exam books and this problem sheet when
you leave
QualExam-F07Fall 2007
Fluid Mechanics 1
A cylindrical annular flow with the inner cylinder rotating at a constant speed ωωωω and
the outer cylinder stationary is shown in the figure below The radii of the outer and
inner cylinders are Ro and Ri respectively
(1) Express the velocity along the wall in terms of the dimensions rotating
speed=ωωωω and the fluid properties viscosity=micromicromicromicro and density=ρρρρ
(2) What is the power needed to move per unit depth Assume Ro ndash Ri ltlt Ro
(3) For SAE 30 oil at 20oC with Ro=10cm Ri=9cm and ωωωω=900rpm calculate
the power
[Hint] The equi-dimensional ordinary differential equation of the function fI
frdquo + (1r)frsquo ndash(1r2)f = 0
has a form of the general solution in the form of f1=C1r and f2=C2r
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 12
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Thermal Science Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Fluid Mechanics 3 problems ( ) ( ) ( )
Thermodynamics 3 problems ( ) ( ) ( )
Heat Transfer 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your assigned number and
NOT your name on each book Submit both exam books and this problem sheet when
you leave
QualExam-F07Fall 2007
Fluid Mechanics 1
A cylindrical annular flow with the inner cylinder rotating at a constant speed ωωωω and
the outer cylinder stationary is shown in the figure below The radii of the outer and
inner cylinders are Ro and Ri respectively
(1) Express the velocity along the wall in terms of the dimensions rotating
speed=ωωωω and the fluid properties viscosity=micromicromicromicro and density=ρρρρ
(2) What is the power needed to move per unit depth Assume Ro ndash Ri ltlt Ro
(3) For SAE 30 oil at 20oC with Ro=10cm Ri=9cm and ωωωω=900rpm calculate
the power
[Hint] The equi-dimensional ordinary differential equation of the function fI
frdquo + (1r)frsquo ndash(1r2)f = 0
has a form of the general solution in the form of f1=C1r and f2=C2r
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 13
Fluid Mechanics 1
A cylindrical annular flow with the inner cylinder rotating at a constant speed ωωωω and
the outer cylinder stationary is shown in the figure below The radii of the outer and
inner cylinders are Ro and Ri respectively
(1) Express the velocity along the wall in terms of the dimensions rotating
speed=ωωωω and the fluid properties viscosity=micromicromicromicro and density=ρρρρ
(2) What is the power needed to move per unit depth Assume Ro ndash Ri ltlt Ro
(3) For SAE 30 oil at 20oC with Ro=10cm Ri=9cm and ωωωω=900rpm calculate
the power
[Hint] The equi-dimensional ordinary differential equation of the function fI
frdquo + (1r)frsquo ndash(1r2)f = 0
has a form of the general solution in the form of f1=C1r and f2=C2r
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 14
Fluid Mechanics 2
A cylindrical rod rests on a wall of 45deg A gate is mounted on the left top side of
the rod to hold water Compute the horizontal and vertical forces due to the water
acting on the 6-ft-diameter cylindrical rod per unit width (1-ft)
612rsquo
A B
C
D
088rdquo 45deg
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 15
Fluid Mechanics 3
A flow field is given by kyjzyixv ˆ)3(ˆ2ˆ2 22 +minusminus=r
bull Show that the flow field is irrotational
bull Derive an expression for the velocity potential Ф within an arbitrary
constant
bull If ξ is a rather complicated path from (0 0 0) to (0 0 4) use Ф to
compute the integral int bull= RdvIrr
over ξ where kzjyixR ˆˆˆ ++=r
is the
position vector of a point on the curve
bull What is the value of I if the integration is performed over a closed
path Do not repeat the calculations performed above to get to the
answer Hint use a well known theorem
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 16
Thermodynamics 1
Refrigerant 134a enters an insulated compressor operating at steady state as saturated
vapor at -10degC at a rate of 18 kgmin At the compressor exit the pressure of the
refrigerant is 5 bar Kinetic and potential energy effects can be neglected If the rate
of entropy production must be kept less than 04842 kJkmin determine the possible
range of values for isentropic compressor efficiency
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 17
Thermodynamics 2
A turbojet engine operates between pressure limits of 5 and 50 psia The inlet air
temperature to the compressor is -40degF and the upper temperature limit for the
engine is 2000degF Calculate the thrust for 1 lbmsec of air flow assuming
isentropic compression and expansion and an inlet velocity of 300 ftsec Assume
constant specific heats Also calculate the heat input per pound mass of air
Inlet
AIR
Exhaust
gas
Burner
QH
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 18
Thermodynamics 3
A liquid-vapor mixture of water with a mass of 03 kg at 150oC occupies an
insulated tank with a volume of 01 m3 Water vapor (and vapor alone) is removed
from the tank until the temperature is 140oC Determine the amount of water that is
removed during the process
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 19
Heat Transfer 1
The temperature of a gas stream is to be measured by a thermocouple whose junction
can be approximated as a 1-mm-diameter sphere The properties of the junction are
k=35 Wm-degC ρ=8500 kgm3 and Cp=320 Jkg-degC and the convection heat transfer
coefficient between the junction and the gas is h=210 Wm2-degC Determine how long
it will take for the thermocouple to read 99 of the initial temperature difference
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 20
Heat Transfer 2
A liquid metal flowing with uniform velocity V through a pipe of periphery P and
cross section A is electrically heated at the rate of u primeprimeprime over a length of l of the pipe
The inlet temperature of the liquid is equal to the ambient temperature Tinfin The
outside heat transfer coefficient is h Neglecting the effect of axial conduction and
you should use the lumped temperature across the cross-sectional area of the pipe
for part (a)
(a) Find the steady axial temperature distribution of the liquid metal
(b) The flow of the liquid metal is suddenly stopped because of a pump
failure Find the unsteady temperature of the liquid metal Hint treat
entire heating region as a single control volume
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 21
Heat Transfer 3
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 22
MECHANICAL ENGINEERING DEPARTMENT
PhD Qualifying Exam
Part II
Area of Concentration
Machine Design Stem
Open BookNotes
November 16 2007
Friday
100 pm ndash 500 pm
Enter problem number(s)
The problems are that you selected
Machine Design 3 problems ( ) ( ) ( )
Kinematics amp Dynamics 3 problems ( ) ( ) ( )
Controls amp Vibration 3 problems ( ) ( ) ( )
The student should select 6 problems out of 9 problems given here Write the problem
numbers that you selected in ( ) above Also circle the problems that you choose on
each problem sheet Choose at least one problem from each category listed above
Use one exam book (blue book) for each problem Include your student ID number
and NOT your name on each book Submit both exam books and this problem sheet
when you leave
QualExam-F07Fall 2007
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 23
Machine Design 1
The figure fellow shows a vehicular jack which is to be designed to support a maximum load of 5000
Newtons The link angle θ varies from 15 to 70 deg The links are 300 mm long Using an assumed
FOS and a suitable cross-section for the links determine the required standard size for the links
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 24
Machine Design 2
The figure below shows portion of a pump that is gear driven at uniform load and speed The shaft is
made of AISI 1045 cold-drawn steel and is supported by bearings mounted in the pump housing
The forces acting on the gear are shown below Find the factor of safety with respect to fatigue
failure at the fillet
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 25
Machine Design 3
For the C-clamp shown below the operator can comfortably exert a 20 lb force at the end of the
handle which creates a clamping force of W = 1000 lb The screw has American Standard
Threads (2θ = 60deg) with 13 threads per inch (single-threaded) The outside diameter is 050 inch
The root diameter and root area are 04001 inch and 01257 inch2 respectively Knowing that dc
= 050 inch micro t = 012 and microc = 025 determine the required handle length L
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 26
Kinematics amp Dynamics 1
The rotations of an airplane about a set of xyz axes attached to the airplane are termed the roll
rate wx the pitching rate wy and the yaw rate wz A passenger on a jumbo jet 30 m behind and 2
m above the center of mass G of the airplane is walking at a constant rate of 1 msec Determine
the difference between the acceleration that this passenger experiences and the acceleration that
the center of mass of the airplane undergoes if the roll rate is 05 radsec the pitching rate is -03
radsec and the yaw rate is 01 radsec All rotation rates are constant
Show all of your work
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 27
Kinematics amp Dynamics 2
The two bars are released from rest at the position θ
Determine their angular velocities at the instant they
become horizontal Neglect the mass of the roller at C
Each bar has a mass m and length L
θ θ
A
B
C
L L
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 28
Kinematics amp Dynamics 3
For the 1-DOF mechanism shown below
(a) Derive the loop equations and identify the known and unknowns in these equations
(b) Derive the velocity equations and identify the known and unknowns in these equations
(c) Derive the acceleration equations Identify the known and unknowns in these equations
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 29
Controls amp Vibration 1
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 30
Controls amp Vibration 2
Consider the following closed-loop control system
1) Determine the system type with respect to the disturbance input D(s)
2) Determine the sensitivity of the closed-loop transfer function T(s) from D(s) to Y(s) to
changes in the parameter A ie ( )T s
AS
3) Let D(s) = 0 determine the steady state error eSS for a unit ramp reference input ie R(s)
2
1( )R s
s====
4) Let D(s) = 0 determine the sensitivity of the steady state error eSS for unit ramp reference
input with respect to changes in K ie SSe
AS
R(s) Y(s)
+ minus
( 1)
A
s sτ ++++ K
+
+
D(s)
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m
Page 31
Controls amp Vibration 3
Find the natural frequencies and modes shapes of the vibrating system shown in the figure below
The following data applies m1 = 1 kg m2 = 2 kg m3 = 3 kg k1 = 300 Nm k2 = 500 Nm k3 =
200 Nm 1 = 075 m